MIDGET GAS TURBINE
    1.
    发明申请
    MIDGET GAS TURBINE 失效
    中空气体涡轮机

    公开(公告)号:US20080231051A1

    公开(公告)日:2008-09-25

    申请号:US10379805

    申请日:2003-03-06

    申请人: Akira Toriyama

    发明人: Akira Toriyama

    摘要: The present invention provides a midget gas turbine has:a casing;an irregular-shaped hollow disk rotationally attached to a casing; said irregular-shaped hollow disk having in a hollow portion constituting a bursiform space having a closed peripheral portion in which a guiding vane is provided, and having a radius changing with respect to the circumferential direction;a fuel conduit provided from a central portion towards a portion of the outer peripheral portion of the irregular-shaped hollow disk and communicated with a fuel nozzle provided in the vicinity of the outer peripheral portion of the irregular-shaped hollow disk; andat least two combustion chambers each comprising a mixing portion for mixing a fuel injected from the fuel nozzle with an external air centrifugally compressed by the guiding vane, a combustor and a combustion gas discharge nozzle portion, said combustion chambers being provided at rotationally symmetric positions at the outer peripheral portion of the irregular-shaped hollow disk where the radius becomes maximum;wherein an external air taken in the hollow portion of the irregular-shaped hollow disk is compressed by the guiding vane, supplied to the combustion chambers, mixed with a fuel supplied from the fuel conduit to be burnt, and a combustion gas discharged from the combustion gas discharge nozzle is discharged towards a substantially circumferential direction of the irregular-shaped hollow disk, whereby the irregular shaped hollow disk is driven by the reaction of the combustion gas.

    摘要翻译: 本发明提供了一种小型燃气轮机,具有:壳体; 旋转地附接到壳体的不规则形状的中空盘; 所述不规则形状的中空盘具有中空部分,该中空部分构成具有闭合周边部分的布袋状空间,其中设置有引导叶片,并且具有相对于圆周方向改变的半径; 燃料导管,其从中心部朝向所述不规则形状的中空盘的外周部的一部分设置,并与设置在所述不规则形状的中空盘的外周部附近的燃料喷嘴连通; 以及至少两个燃烧室,每个燃烧室包括混合部分,用于将从燃料喷嘴喷射的燃料与由引导叶片离心压缩的外部空气混合,燃烧器和燃烧气体排放喷嘴部分,所述燃烧室设置在旋转对称位置 在半径变得最大的不规则形状的中空盘的外周部分; 取入在不规则形状的中空盘的中空部分的外部空气被供给到燃烧室的引导叶片压缩,与从燃烧管道供给的燃料混合,从燃烧排出的燃烧气体 气体排出喷嘴朝向不规则形状的中空盘的大致圆周方向排出,由此通过燃烧气体的反应来驱动不规则形状的中空盘。

    Honeycomb type solid electrolytic fuel cell
    2.
    发明授权
    Honeycomb type solid electrolytic fuel cell 失效
    蜂窝型固体电解质燃料电池

    公开(公告)号:US07507489B2

    公开(公告)日:2009-03-24

    申请号:US10528116

    申请日:2004-03-12

    申请人: Akira Toriyama

    发明人: Akira Toriyama

    IPC分类号: H01M8/12

    摘要: A SOFC type fuel cell being small in size and large in output while providing good efficiency and being excellent in starting characteristics and load variation characteristics, is presented. A honeycomb type solid-oxide fuel cell is formed of a honeycomb structural body having square cell in cross section, wherein cells adjacent to wall surfaces constituting a fuel pole cell (a) function as air pole cells (b) and cells adjacent to the corners of wall surfaces of the fuel pole cell and adjacent to wall surfaces constituting air pole cell function as cooling air cells (c), whereby fuel pole cells, air pole cells and cooling air cells are arranged in longitudinal and lateral rows so that cells of the same type appear in every other location.

    摘要翻译: 提出了一种尺寸小,输出大的SOFC型燃料电池,同时具有良好的效率和优异的起动特性和负载变化特性。 蜂窝型固体氧化物燃料电池由具有方形电池的蜂窝状结构体的横截面形成,其中与构成燃料极电池(a)的壁面相邻的电池用作气柱电池(b)和与角部相邻的电池 燃料极单元的壁表面和构成空气极单元的壁表面相邻的壁表面用作冷却空气室(c),由此燃料极单元,空气极单元和冷却空气单元布置在纵向和横向行中,使得单元 每个其他位置都会显示相同的类型。

    Midget gas turbine
    4.
    发明授权
    Midget gas turbine 失效
    小型燃气轮机

    公开(公告)号:US07462948B2

    公开(公告)日:2008-12-09

    申请号:US10379805

    申请日:2003-03-06

    申请人: Akira Toriyama

    发明人: Akira Toriyama

    IPC分类号: H20P9/00

    摘要: The present invention provides a midget gas turbine has: a casing; an irregular-shaped hollow disk rotationally attached to a casing; said irregular-shaped hollow disk having in a hollow portion constituting a bursiform space having a closed peripheral portion in which a guiding vane is provided, and having a radius changing with respect to the circumferential direction; a fuel conduit provided from a central portion towards a portion of the outer peripheral portion of the irregular-shaped hollow disk and communicated with a fuel nozzle provided in the vicinity of the outer peripheral portion of the irregular-shaped hollow disk; and at least two combustion chambers each comprising a mixing portion for mixing a fuel injected from the fuel nozzle with an external air centrifugally compressed by the guiding vane, a combustor and a combustion gas discharge nozzle portion, said combustion chambers being provided at rotationally symmetric positions at the outer peripheral portion of the irregular-shaped hollow disk where the radius becomes maximum; wherein an external air taken in the hollow portion of the irregular-shaped hollow disk is compressed by the guiding vane, supplied to the combustion chambers, mixed with a fuel supplied from the fuel conduit to be burnt, and a combustion gas discharged from the combustion gas discharge nozzle is discharged towards a substantially circumferential direction of the irregular-shaped hollow disk, whereby the irregular shaped hollow disk is driven by the reaction of the combustion gas.

    摘要翻译: 本发明提供了一种小型燃气轮机,具有:壳体; 旋转地附接到壳体的不规则形状的中空盘; 所述不规则形状的中空盘具有中空部分,该中空部分构成具有闭合周边部分的布袋状空间,其中设置有引导叶片,并且具有相对于圆周方向改变的半径; 燃料导管,其从中心部朝向所述不规则形状的中空盘的外周部的一部分设置,并与设置在所述不规则形状的中空盘的外周部附近的燃料喷嘴连通; 以及至少两个燃烧室,每个燃烧室包括混合部分,用于将从燃料喷嘴喷射的燃料与由引导叶片离心压缩的外部空气混合,燃烧器和燃烧气体排放喷嘴部分,所述燃烧室设置在旋转对称位置 在半径变得最大的不规则形状的中空盘的外周部分; 取入在不规则形状的中空盘的中空部分的外部空气被供给到燃烧室的引导叶片压缩,与从燃烧管道供给的燃料混合,从燃烧排出的燃烧气体 气体排出喷嘴朝向不规则形状的中空盘的大致圆周方向排出,由此通过燃烧气体的反应来驱动不规则形状的中空盘。

    Honeycomb type solid electrolytic fuel cell

    公开(公告)号:US20060051641A1

    公开(公告)日:2006-03-09

    申请号:US10528116

    申请日:2004-03-12

    申请人: Akira Toriyama

    发明人: Akira Toriyama

    IPC分类号: H01M8/04 H01M8/10

    摘要: A SOFC type fuel cell being small in size and large in output while providing good efficiency and being excellent in starting characteristics and load variation characteristics, is presented. A honeycomb type solid-oxide fuel cell is formed of a honeycomb structural body having square cell in cross section, wherein cells adjacent to wall surfaces constituting a fuel pole cell (a) function as air pole cells (b) and cells adjacent to the corners of wall surfaces of the fuel pole cell and adjacent to wall surfaces constituting air pole cell function as cooling air cells (c), whereby fuel pole cells, air pole cells and cooling air cells are arranged in longitudinal and lateral rows so that cells of the same type appear in every other location.